US7134852B1 - Seal member for vortex compressor - Google Patents
Seal member for vortex compressor Download PDFInfo
- Publication number
- US7134852B1 US7134852B1 US11/333,369 US33336906A US7134852B1 US 7134852 B1 US7134852 B1 US 7134852B1 US 33336906 A US33336906 A US 33336906A US 7134852 B1 US7134852 B1 US 7134852B1
- Authority
- US
- United States
- Prior art keywords
- vortex
- stationary
- rotatable
- groove
- seal member
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 230000006835 compression Effects 0.000 claims abstract description 11
- 238000007906 compression Methods 0.000 claims abstract description 11
- 239000003507 refrigerant Substances 0.000 abstract description 17
- 238000004378 air conditioning Methods 0.000 description 2
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/02—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
- F04C18/0207—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
- F04C18/0215—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form where only one member is moving
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C27/00—Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
- F04C27/005—Axial sealings for working fluid
Definitions
- the present invention relates to a seal member installed in the end surface of each of the stationary vortex body and rotatable vortex body.
- a conventional vortex compressor includes a casing in which a compression chamber and an expelling chamber are defined and separated by a stationary vortex body.
- the refrigerant is introduced into the compression chamber via an inlet and the rotatable vortex body is rotated relative to the stationary vortex body to compress the refrigerant.
- the pressure between the base board and vortex surface of the stationary vortex body and the rotatable vortex body suddenly increases such that leakage might happen in axial direction. The leakage is worse when the vortex surface is worn out. This results in less efficiency for the refrigerant in the whole air-conditioning system.
- a vortex groove 81 is defined in the end surface 8 of the stationary and rotatable vortex bodies and a seal member 9 is engaged with the groove 81 so as to improved the leakage described in the above-mentioned air-conditioning system.
- the present invention intends to provide a seal member which includes a stepped surface defined in the first end thereof so that when the compressor is activated, the refrigerant enters the gap between the seals and the grooves to push the seal members toward the vortex boards so that the pressure is maintained. By this way, the efficiency for the compressor can be increased.
- the present invention relates to a vortex compressor which comprises a casing in which a stationary vortex body and a rotatable vortex body are located so as to define a compression chamber and an expelling chamber with the stationary vortex body located between the two chambers.
- the stationary vortex body and the rotatable vortex body are located in the compression chamber.
- Each of the stationary vortex body and the rotatable vortex body has a base board and a vortex portion extends from the base board.
- a vortex groove is defined in an end surface of each of the vortex portion and a seal member is engaged with the vortex groove.
- the vortex groove includes a start end which is located close to the base board.
- Each of the seal members includes a cut-off portion defined in a distal end thereof and located close to the start end of the vortex groove.
- the cut-off portion faces an inside of the vortex groove. The refrigerant enters the gap between the cut-off portion of the seals and the grooves to push the seal members toward the vortex boards when the compressor is activated.
- FIG. 1 is a cross sectional view of the compressor
- FIG. 2 is a cross sectional view along line 2 — 2 in FIG. 1 ;
- FIG. 3 shows the seal member engaged with the vortex groove
- FIG. 4 shows refrigerant enters the gap between the seal member and the inside of the vortex groove
- FIG. 5 shows the base board, the vortex portion, and the seal member engaged with the vortex groove
- FIG. 6 shows a second embodiment of the seal member
- FIG. 7 shows a third embodiment of the seal member
- FIG. 8 is a conventional seal member and the vortex groove of the vortex body.
- the vortex compressor of the present invention comprises a casing 1 in which a stationary vortex body 2 and a rotatable vortex body 3 are located.
- the rotatable vortex body 3 is rotatable relative to the stationary vortex body 2 .
- a compression chamber 4 and an expelling chamber 5 are defined in the casing 1 and separated by the stationary vortex body 2 .
- the stationary vortex body 2 and the rotatable vortex body 3 are located in the compression chamber 4 .
- Each of the stationary vortex body 2 and the rotatable vortex body 3 has a base board 21 / 31 and a vortex portion 22 / 32 extends from the base board 21 / 31 .
- a vortex groove 23 / 33 is defined in an end surface of each of the vortex portion 22 / 32 .
- a seal member 6 / 7 is engaged with the vortex groove 23 / 33 .
- the vortex groove 23 / 33 includes a start end 24 / 34 which is located close to the base board 21 / 31 .
- Each of the seal members 6 / 7 includes a cut-off portion defined in a distal end 61 / 71 thereof which is located close to the start end 24 / 34 of the vortex groove 23 / 33 .
- a gap 25 / 35 is defined between the distal end 61 / 71 of the seal member 6 / 7 and the start end 24 / 34 of the vortex groove 23 / 33 as shown in FIGS. 3 and 4 and a stepped surface 62 / 72 is defined in the cut-off portion and faces an inside of the vortex groove 23 / 33 .
- the refrigerant When the compressor is activated, the refrigerant enters into the start end 24 / 34 of the vortex groove 23 / 33 due to higher pressure and applies a force to the stepped surface 62 / 72 , the distal end 61 / 71 of the seal member 6 / 7 is then lifted upward slightly and the refrigerant then enters the gap between the seal member 6 / 7 and the inside of the vortex groove 23 / 33 till the final end 231 / 331 of the vortex groove 23 / 33 .
- the seal member 6 / 7 is pushed by the refrigerant to contact against the base board 21 / 31 so as to effectively seal the base board 21 / 31 and the vortex portion 22 / 32 .
- the compression ratio can be maintained and even if the seal member 6 / 7 is slightly worn out, the seal member 6 / 7 still seals the gap by the refrigerant.
- FIG. 6 discloses a second embodiment of the seal member 6 / 7 wherein the cut-off portion is an inclined surface 63 / 73 .
- the compressor When the compressor is activated, the refrigerant enters into the start end 24 / 34 of the vortex groove 23 / 33 due to higher pressure and applies a force to the inclined surface 63 / 73 , the distal end 61 / 721 of the seal member 6 / 7 is then lifted upward slightly and the refrigerant then enters the gap between the seal member 6 / 7 and the inside of the vortex groove 23 / 33 till the final end 231 / 331 of the vortex groove 23 / 33 .
- the seal member 6 / 7 is pushed by the refrigerant to contact against the base board 21 / 31 so as to effectively seal the base board 21 / 31 and the vortex portion 22 / 32 .
- FIG. 7 shows a third embodiment of the seal member wherein the cut-off portion is an inclined a combination surface 64 / 74 which is composed of an inclined section 641 / 741 and a vertical section 642 / 742 .
- the compressor When the compressor is activated, the refrigerant enters into the start end 24 / 34 of the vortex groove 23 / 33 due to higher pressure and applies a force to the combination surface 64 / 74 , the distal end 61 / 71 of the seal member 6 / 7 is then lifted upward slightly and the refrigerant then enters the gap between the seal member 6 / 7 and the inside of the vortex groove 23 / 33 till the final end 231 / 331 of the vortex groove 23 / 33 .
- the seal member 6 / 7 is pushed by the refrigerant to contact against the base board 21 / 31 so as to effectively seal the base board 21 / 31 and the vortex portion 22 / 32 .
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Compressor (AREA)
Abstract
Description
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/333,369 US7134852B1 (en) | 2006-01-18 | 2006-01-18 | Seal member for vortex compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/333,369 US7134852B1 (en) | 2006-01-18 | 2006-01-18 | Seal member for vortex compressor |
Publications (1)
Publication Number | Publication Date |
---|---|
US7134852B1 true US7134852B1 (en) | 2006-11-14 |
Family
ID=37397586
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/333,369 Expired - Fee Related US7134852B1 (en) | 2006-01-18 | 2006-01-18 | Seal member for vortex compressor |
Country Status (1)
Country | Link |
---|---|
US (1) | US7134852B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009038138A1 (en) * | 2007-09-21 | 2009-03-26 | Mitsubishi Heavy Industries, Ltd. | Scroll compressor |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01121582A (en) * | 1987-11-06 | 1989-05-15 | Sanyo Electric Co Ltd | Scroll type compressor |
US4869658A (en) * | 1987-02-27 | 1989-09-26 | Iwata Air Compressor Manufacturing Company Limited | Prevention against shifting of tip seal of scroll compressor |
JPH0311101A (en) * | 1989-06-09 | 1991-01-18 | Iwata Tosouki Kogyo Kk | Scroll fluid machine |
JPH03246389A (en) * | 1990-02-23 | 1991-11-01 | Sanden Corp | Scroll compressor |
JPH06272679A (en) * | 1993-03-17 | 1994-09-27 | Tokico Ltd | Scroll fluid machine |
JP2002031069A (en) * | 2000-07-19 | 2002-01-31 | Keihin Corp | Scroll type compressor |
-
2006
- 2006-01-18 US US11/333,369 patent/US7134852B1/en not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4869658A (en) * | 1987-02-27 | 1989-09-26 | Iwata Air Compressor Manufacturing Company Limited | Prevention against shifting of tip seal of scroll compressor |
JPH01121582A (en) * | 1987-11-06 | 1989-05-15 | Sanyo Electric Co Ltd | Scroll type compressor |
JPH0311101A (en) * | 1989-06-09 | 1991-01-18 | Iwata Tosouki Kogyo Kk | Scroll fluid machine |
JPH03246389A (en) * | 1990-02-23 | 1991-11-01 | Sanden Corp | Scroll compressor |
JPH06272679A (en) * | 1993-03-17 | 1994-09-27 | Tokico Ltd | Scroll fluid machine |
JP2002031069A (en) * | 2000-07-19 | 2002-01-31 | Keihin Corp | Scroll type compressor |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009038138A1 (en) * | 2007-09-21 | 2009-03-26 | Mitsubishi Heavy Industries, Ltd. | Scroll compressor |
JP2009074461A (en) * | 2007-09-21 | 2009-04-09 | Mitsubishi Heavy Ind Ltd | Scroll compressor |
EP2192304A1 (en) * | 2007-09-21 | 2010-06-02 | Mitsubishi Heavy Industries, Ltd. | Scroll compressor |
US20100172780A1 (en) * | 2007-09-21 | 2010-07-08 | Mitsubishi Heavy Industries, Ltd. | Scroll Compressor |
US8152501B2 (en) | 2007-09-21 | 2012-04-10 | Mitsubishi Heavy Industries, Ltd. | Scroll compressor for preventing performance deterioration and variation due to gas leakage |
EP2192304A4 (en) * | 2007-09-21 | 2015-04-22 | Mitsubishi Heavy Ind Ltd | Scroll compressor |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: HE JHANG ENVIRONMENTAL TECHNOLOGY CO., LTD., TAIWA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:LAI, CHIN-LIANG;REEL/FRAME:017216/0078 Effective date: 20051121 |
|
AS | Assignment |
Owner name: HOLIN ELECTRIC LTD., TAIWAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:HE JHANG ENVIRONMENTAL TECHNOLOGY CO., LTD.;REEL/FRAME:018330/0910 Effective date: 20060829 |
|
AS | Assignment |
Owner name: HENG SHENG PRECISION TECH. CO., LTD., TAIWAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:HOLIN ELECTRIC LTD.;REEL/FRAME:018461/0812 Effective date: 20061018 |
|
FPAY | Fee payment |
Year of fee payment: 4 |
|
FPAY | Fee payment |
Year of fee payment: 8 |
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FEPP | Fee payment procedure |
Free format text: MAINTENANCE FEE REMINDER MAILED (ORIGINAL EVENT CODE: REM.) |
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LAPS | Lapse for failure to pay maintenance fees |
Free format text: PATENT EXPIRED FOR FAILURE TO PAY MAINTENANCE FEES (ORIGINAL EVENT CODE: EXP.); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY |
|
STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |
|
FP | Lapsed due to failure to pay maintenance fee |
Effective date: 20181114 |